Insert and standoff design for a gas turbine engine vane
US10280793B2 · kind B2 · utility
4Cited by
9References
20Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Aug 28, 2014 |
| Grant date | May 7, 2019 |
| Priority date | — |
| Expiry date | Dec 30, 2035 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2260/201
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a platform, an airfoil that extends from the platform, and an insert positioned such that a first portion of the insert extends relative to a surface of the platform and a second portion extends inside the airfoil. A standoff supports the insert above the surface.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.